Research Catalog
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Displaying 1-15 of 15 results
A method for guiding efflux air from a fan-in-wing model into a discharge duct; test report, by U. W. Schaub and R. J. Rimmer.
- Text
- [Ottawa, National Research Council of Canada, 1970]
- 1970
- 1 Item
Item details Format Call Number Item Location Text JSK 74-291 no. 508 (Feb. 1970) Offsite Low noise research fan stage design [microform] / David E. Hobbs ... [et al.].
- Text
- [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
- 1995
Propulsion/airframe interference for ducted propfan engines with ground effect [microform] / Abdollah Arabshahi and Ramesh Pankajakshan.
- Text
- [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
- 1994
Active control of fan noise--feasibility study [microform].
- Text
- [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1994- ]
- 1994-present
Comparison of predicted low speed fan rotor/stator interaction modes to measured [microform] / Daniel L. Sutliff, James Bridges, Edmane Envia.
- Text
- Washington, DC : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
- 1997
Advanced low-noise research fan stage design [microform] / Robert Neubert ... [et al.] ; prepared under contract NAS3-26618.
- Text
- [Washington, DC] : National Aeronautics and Space Administration, Lewis Research Center ; Available from Springfield, VA : National Technical Information Service, distributor, [1997]
- 1997
Boeing 18-inch fan rig broadband noise test [microform] / Ulrich Ganz ... [et al.].
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
- 1998
Model engine performance measurement from force balance instrumentation [microform] / Robert J. Jeracki.
- Text
- [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
- 1998
Final technical report for Euler/Navier-Stokes solvers applied to ducted fan configurations [microform] : NASA grant number NAG3-1230 : grant duration, December 20, 1990 to December 20, 1996 / Theo G. Keith, Jr., principal investigator; Rakesh Srivastava, co-principal investigator.
- Text
- [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
- 1997
Final technical report for aeroelastic analysis of propulsion systems [microform] : NASA grant number NAG3-1068 : grant duration, August 16, 1989 to December 9, 1993 / Theo G. Keith, Jr. & Aparajit Mahajan.
- Text
- Toledo, Ohio : Dept. of Mechanical, Industrial and Manufacturing Engineering, University of Toledo ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
- 1996
Coupling of low speed fan stator vane unsteady pressures to duct modes [microform] : measured versus predicted / Daniel L. Sutliff, Laurence J. Heidelberg and Edmane Envia.
- Text
- [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Springfield, VA : National Technical Information Service, distributor, [1999]
- 1999
Advanced nacelle acoustic lining concepts development [microform] / G. Bielak ... [et al.].
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 2002]
- 2002
- 1 Resource
Available Online
http://purl.access.gpo.gov/GPO/LPS60573A mode propagation database suitable for code validation utilizing the NASA Glenn advanced noise control fan and artificial sources / Daniel L. Sutliff.
- Text
- Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, April 2014.
- 2014-4
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo53745Computational aerodynamic simulations of an 840 ft/sec tip speed advanced ducted propulsor fan system model for acoustic methods assessment and development / Daniel L. Tweedt.
- Text
- Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, October 2014.
- 2014-10
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo55838Comparison of predicted low speed fan rotor/stator interaction modes to measured / Daniel L. Sutliff, James Bridges, Edmane Envia.
- Text
- Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, May 1996.
- 1996-5
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo72616
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